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Airspeed.mat
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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C_code24.txt
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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ConvertToC.m
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EKF: Update derivation scripts and outputs
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2016-03-11 11:03:43 +11:00 |
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ConvertToM.m
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EKF: Update derivation scripts and outputs
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2016-03-11 11:03:43 +11:00 |
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Drag.mat
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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EulToQuat.m
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Add derivation script files for inertial nav EKF
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2015-11-03 12:24:43 +11:00 |
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GenerateNavFilterEquations.m
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Matlab: Improve efficiency of odometry derivation
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2017-06-03 12:39:24 +10:00 |
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H_LOSX.c
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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H_LOSY.c
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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H_VELX.c
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EKF: Clean up auto-code files for body frame velocity measurements
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2017-03-06 09:01:46 +11:00 |
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H_VELY.c
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EKF: Clean up auto-code files for body frame velocity measurements
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2017-03-06 09:01:46 +11:00 |
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H_VELZ.c
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EKF: Clean up auto-code files for body frame velocity measurements
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2017-03-06 09:01:46 +11:00 |
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K_LOSX.c
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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K_LOSY.c
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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K_VELX.c
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EKF: Clean up auto-code files for body frame velocity measurements
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2017-03-06 09:01:46 +11:00 |
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K_VELY.c
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EKF: Clean up auto-code files for body frame velocity measurements
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2017-03-06 09:01:46 +11:00 |
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K_VELZ.c
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EKF: Clean up auto-code files for body frame velocity measurements
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2017-03-06 09:01:46 +11:00 |
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M_code24.txt
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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Magnetometer.mat
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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NormQuat.m
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Add derivation script files for inertial nav EKF
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2015-11-03 12:24:43 +11:00 |
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OptimiseAlgebra.m
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Add derivation script files for inertial nav EKF
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2015-11-03 12:24:43 +11:00 |
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Q_airdata.c
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matlab: add derivation for air data error equations
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2017-08-12 20:59:41 +10:00 |
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Quat2Tbn.m
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Add derivation script files for inertial nav EKF
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2015-11-03 12:24:43 +11:00 |
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QuatDivide.m
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Add derivation script files for inertial nav EKF
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2015-11-03 12:24:43 +11:00 |
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QuatErrTransferEquations.m
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EKF: derive auto-code for quaternion state covariance initialisation
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2016-05-17 12:28:58 +10:00 |
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QuatMult.m
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Add derivation script files for inertial nav EKF
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2015-11-03 12:24:43 +11:00 |
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QuatToEul.m
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Add derivation script files for inertial nav EKF
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2015-11-03 12:24:43 +11:00 |
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RotToQuat.m
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Add derivation script files for inertial nav EKF
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2015-11-03 12:24:43 +11:00 |
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SaveScriptCode.m
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EKF: Update derivation scripts and outputs
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2016-03-11 11:03:43 +11:00 |
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Sideslip.mat
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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StateAndCovariancePrediction.mat
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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StatePrediction.mat
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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SymbolicOutput24.mat
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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SymbolicOutput24.txt
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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Tbn_312.c
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matlab: Add scripts to calculate rotation conversions for 321 or 312 Euler sequences
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2017-07-21 10:22:17 +10:00 |
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Tbn_321.c
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matlab: Add scripts to calculate rotation conversions for 321 or 312 Euler sequences
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2017-07-21 10:22:17 +10:00 |
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Tbn_quat.c
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matlab: Add scripts to calculate rotation conversions for 321 or 312 Euler sequences
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2017-07-21 10:22:17 +10:00 |
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calcH_YAW312.c
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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calcH_YAW321.c
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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calcMAGD.c
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EKF: Include all output files generated by derivation script
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2016-04-05 22:23:37 +02:00 |
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derive_air_data_errors.m
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matlab: add derivation for air data error equations
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2017-08-12 20:59:41 +10:00 |
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fix_c_code.m
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EKF: Update derivation scripts and outputs
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2016-03-11 11:03:43 +11:00 |
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polar2cart_cov.m
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scripts: derive conversion from polar to cartesian wind state covariance
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2016-08-11 15:26:21 +02:00 |
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quat2yaw312.m
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matlab: Allow replay to handle late start GPS data in log
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2017-07-24 16:34:50 +10:00 |
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quat2yaw321.m
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matlab: Fix derivation for 321 Euler rotation sequence
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2017-07-21 10:48:54 +10:00 |
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quatCovMat.c
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EKF: derive auto-code for quaternion state covariance initialisation
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2016-05-17 12:28:58 +10:00 |
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rotVarVec.c
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EKF: Add matlab derivation for calculation of rotation vector variance
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2016-05-17 10:56:19 +10:00 |
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temp1.mat
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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temp2.mat
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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temp3.mat
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EKF: update derivation files
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2016-05-05 21:23:03 +10:00 |
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test_output_filter_gains.m
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EKF: add matlab script to test complementary filter gains
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2016-04-30 11:05:03 +10:00 |
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yaw_input_312.c
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matlab: Add scripts to calculate rotation conversions for 321 or 312 Euler sequences
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2017-07-21 10:22:17 +10:00 |
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yaw_input_321.c
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matlab: Fix derivation for 321 Euler rotation sequence
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2017-07-21 10:48:54 +10:00 |
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